EXPERIMENTAL INVESTIGATION OF A 2-D AIR AUGMENTED ROCKET: HIGH PRESSURE RATIO AND TRANSIENT FLOW-FIELDS

EXPERIMENTAL INVESTIGATION OF A 2-D AIR AUGMENTED ROCKET: HIGH PRESSURE RATIO AND TRANSIENT FLOW-FIELDS

A 2-D Air Augmented Rocket, the Cal Poly Air Augmented Rocket (CPAAR) Test Apparatus operating as a mixer-ejector was tested to investigate high stagnation pressure ratio and transient flow fields of an ejector. The primary rocket ejector was supplied with high pressure nitrogen at a maximum chamber...

Full description

Bibliographic Details
Main Author: Sanchez, Josef S
Format: Others
Published: DigitalCommons@CalPoly 2012
Subjects:
Air Augmented Rocket
Supersonic Ejector
Transient Flow
Pressure Ratio
Aerodynamics and Fluid Mechanics
Propulsion and Power
Online Access:https://digitalcommons.calpoly.edu/theses/690
https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1732&context=theses

Internet

https://digitalcommons.calpoly.edu/theses/690
https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1732&context=theses

Similar Items